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GENMAT-1

NORAD 58276 Payload LEO 2023-174W ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
454 km
Apogee
461 km
Inclination
97.4°
Period
93.8 min
Mean Motion
15.36110254 rev/day
TLE Epoch
2026-09-18 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude458 km
Orbital Velocity27,505 km/h
Velocity7.64 km/s
Orbital Period94 minutes
Orbits / Day15.36
Eccentricity0.0005
Semi-Major Axis6,829 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇺🇸 GenMat (United States)
Launch Date
2023-11-11
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
2023-174W
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
GENMAT-1 is an active satellite operated by GenMat (United States), launched on 2023-11-11 from Vandenberg Space Force Base, United States on the Transporter-9 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 454 km and 461 km with an inclination of 97.4°. It travels at approximately 27,505 km/h (7.64 km/s), completing one full orbit every 94 minutes — that’s roughly 15.36 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~1–3 years. Orbital Radar tracks GENMAT-1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
GENMAT-1 orbits at an average altitude of 458 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of GENMAT-1’s average altitude, there are currently 10,102 active payloads and 157 tracked debris or rocket body fragments — notable neighbours include ISS (ZARYA), STARLINK-1017, STARLINK-1039. This makes it one of the more crowded altitude bands, containing roughly 54% of all active satellites. With an inclination of 97.4°, GENMAT-1 passes over latitudes between 97.4°N and 97.4°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. United States operates approximately 13,204 active satellites in total, of which 9,596 share a similar altitude band with GENMAT-1.
❓ Frequently Asked Questions
GENMAT-1 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 458 km altitude. Its 97.4° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 94 minutes, travelling at 27,505 km/h.
GENMAT-1 is operated by GenMat (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 58276. You can track GENMAT-1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
GENMAT-1 was launched on 2023-11-11 from Vandenberg Space Force Base, United States, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks GENMAT-1 (NORAD ID 58276) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
GENMAT-1 travels at approximately 27,505 km/h (17,091 mph) — roughly 7.64 km/s. It completes 15.36 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.